| Analyzed File: | QuadCopter Main Body.ipt |
| Autodesk Inventor Version: | 2022 (Build 260153000, 153) |
| Creation Date: | 4/28/2023, 8:10 AM |
| Study Author: | Grace |
General objective and settings:
Design Objective Single Point Study Type Static Analysis Last Modification Date 4/28/2023, 6:25 AM Model State Master Detect and Eliminate Rigid Body Modes No iProperties
Summary
Author Grace Project
Part Number QuadCopter Main Body Designer Grace Cost $0.00 Date Created 4/27/2023 Status
Design Status WorkInProgress Physical
Material PC/ABS Plastic Density 0.357273 g/cm^3 Mass 0.0489973 kg Area 30992.3 mm^2 Volume 137142 mm^3 Center of Gravity x=3.49722 mm
y=-2.25965 mm
z=0.00540883 mmNote: Physical values could be different from Physical values used by FEA reported below.
Mesh settings:
Avg. Element Size (fraction of model diameter) 0.1 Min. Element Size (fraction of avg. size) 0.2 Grading Factor 1.5 Max. Turn Angle 60 deg Create Curved Mesh Elements Yes Material(s)
Name PC/ABS Plastic General Mass Density 0.357273 g/cm^3 Yield Strength 54.4 MPa Ultimate Tensile Strength 54.1 MPa Stress Young's Modulus 2.78 GPa Poisson's Ratio 0.4 ul Shear Modulus 0.992857 GPa Part Name(s) QuadCopter Main Body.ipt Operating conditions
Force:1
Load Type Force Magnitude 20.000 N Vector X 0.000 N Vector Y -20.000 N Vector Z 0.000 N Selected Face(s)
Bearing Load:1
Load Type Bearing Load Magnitude 20.000 N Vector X 0.000 N Vector Y 20.000 N Vector Z 0.000 N Selected Face(s)
Bearing Load:2
Load Type Bearing Load Magnitude 20.000 N Vector X 0.000 N Vector Y 20.000 N Vector Z 0.000 N Selected Face(s)
Bearing Load:3
Load Type Bearing Load Magnitude 20.000 N Vector X 0.000 N Vector Y 20.000 N Vector Z 0.000 N Selected Face(s)
Bearing Load:4
Load Type Bearing Load Magnitude 20.000 N Vector X 0.000 N Vector Y 20.000 N Vector Z 0.000 N Selected Face(s)
Gravity
Load Type Gravity Magnitude 9810.000 mm/s^2 Vector X 0.000 mm/s^2 Vector Y -9810.000 mm/s^2 Vector Z 0.000 mm/s^2 Selected Face(s)
